|Número de publicación||US7210740 B2|
|Tipo de publicación||Concesión|
|Número de solicitud||US 11/387,241|
|Fecha de publicación||1 May 2007|
|Fecha de presentación||22 Mar 2006|
|Fecha de prioridad||6 Oct 2003|
|También publicado como||EP1670336A2, EP1670337A2, US7159937, US7182403, US7195319, US7201448, US20050121963, US20050168042, US20060181118, US20060208550, US20060214482, WO2005035301A2, WO2005035301A3, WO2005035302A2, WO2005035302A3|
|Número de publicación||11387241, 387241, US 7210740 B2, US 7210740B2, US-B2-7210740, US7210740 B2, US7210740B2|
|Inventores||Sreekanth Chintapudi, Pedro Meneses|
|Cesionario original||B/E Aerospace, Inc.|
|Exportar cita||BiBTeX, EndNote, RefMan|
|Citas de patentes (42), Citada por (4), Clasificaciones (36), Eventos legales (5)|
|Enlaces externos: USPTO, Cesión de USPTO, Espacenet|
This patent application is a divisional of U.S. patent application Ser. No. 10/960,299, filed Oct. 6, 2004, which claims the benefit of U.S. Provisional Patent Application No. 60/509,402, filed Oct. 6, 2003, entitled Airplane Passenger Seat, the content of each is incorporated herein by reference in its entirety for all purposes.
This invention pertains to a reclining chair in general and, more particularly, to a reclining chair for use as a passenger seat in an aircraft.
In order to increase the comfort of a person seated in a chair, manufacturers have long made chairs with a backrest that is capable of reclining several degrees with respect to a vertical position. Today, seats with a reclining backrest are used in homes, offices, and vehicles; including aircraft and buses. While offering greater comfort than a straight back chair, known recliners are limited in that their backrests are, for the most part, not capable of fully reclining to a horizontal position. Although some seats, such as certain aircraft seats, are capable of fully reclining, these seats are constructed so that a space exists between the seat and back cushion when the backrest is fully reclined. Furthermore, the known recliners are incapable of reclining to a fully horizontal position so as to form a flat sleeping surface. For this reason, a chair capable of reclining to a full horizontal position would be an important improvement in the art.
In addition to being able to fully recline to a bed-like sleeping platform, seats that are installed in vehicles such as buses, mobile homes and aircraft must also be able to absorb dynamic loads that may be imparted on the seat as a result of gravitational forces generated by changes in speed and direction of the vehicle. In order to obtain maximum comfort for the occupant in these types of situations, the seat frame must be able to absorb these forces so as to limit their impact on the occupant. Furthermore, under the standards set forth in FAR § 25.562, in order to be certified as airworthy, the seat frame must be able to absorb the forces without separating from the floor of the aircraft in an emergency such as a crash landing. For this reason, a seat that is capable of absorbing dynamic loads imparted on the seat as a result of changes in the direction or speed of a vehicle would be an important improvement in the art.
The invention is directed to a chair comprised of a base assembly, a seat frame located above the base assembly, a seat attached to the seat frame, and a seat back connected to the seat frame. In various embodiments, the seat, in particular an aircraft seat, includes features such as an energy absorbing base assembly, a fully reclining seat back and a seat that increases its angle with respect to the horizontal as the seat back reclines, thereby forcing one back into the seat. The seat and seat back is also capable of achieving a fully horizontal position when the seat back is fully reclined.
These and other advantages of the invention will be apparent from the description of the invention provided herein.
The invention is directed to a reclining chair 10, in particular, a chair 10 for use in a vehicle such as an aircraft or bus. The chair, as shown in
In one embodiment of the invention, each of the base rails 20, 22 has two openings 26, 42. In this version, the first opening 26 is located approximately midway along the length of the base rail 20 and a second opening 42 is located proximal to the second end 34 of the base rail 20.
The first and second leg members 30, 32 of the base rails 20, 22 may be capable of attaching to a floor fitting 44, as shown in
As shown in
When in operation, the angling of the leg members 30, 32 helps the base rails 20, 22 to absorb energy during a dynamic event. This reduces the structural loading on the base rails 20, 22 during pitch and roll, thereby helping to reduce aircraft floor warping in the event of a major dynamic load.
Furthermore, the prongs 46 of the leg members 30, 32 in one embodiment allow the base rail to be attached to an articulating foot fitting similar to the type disclosed in U.S. patent application Ser. No. 10/944,487, filed Sep. 17, 2004, entitled Attachment Assembly for Mounting a Seat to the Floor of a Vehicle, the entire content of which is incorporated herein by reference. This also helps the base rails 20, 22 to absorb dynamic loads by allowing the rail 20, 22 to rotate slightly with respect to the floor of the vehicle in the event of an abrupt stop caused by an emergency or crash.
In yet another version, the first and second leg members 30, 32 are attached to the elongated portion 24 of the base rail 20. In still another version, the second leg member 32 extends from the second end 34 of the base rail 20.
As shown in
When in use, the seat frame 14 is positioned above the base assembly 12, as shown in
A seat back 18 is connected to the seat frame 14, as shown in
As shown in
In one embodiment of the invention, as shown in FIGS. 15 and 23–26, at least one support beam 150 extends between the first and second backrest rails 68, 70. A torque box 152 may also be positioned between the first and second backrest rails 68, 70, as shown in FIGS. 15 and 23–26.
As shown in
The torque box 152 serves as the primary structural member of the seat back 18. Because of its box shape, the torque box 152 is able to transfer shoulder harness induced loading from the backrest rail 68 nearest the harness to the opposite backrest rail 70 in the forward facing static and dynamic test conditions. In contrast to existing seat designs that utilize torque tubes, the torque box 152 has a rectangular cross section that allows for a wider separation between headrest support brackets 168, particularly for a headrest utilizing longer brackets. Furthermore, the torque box 152 provides sufficient space to house an inertial reel (not shown), electric headrest mechanism (not shown) and longer headrest support brackets 168.
When in operation, as the seat back reclines, there is a tendency for the unsupported side of the seat back 18 to drop away from the seat occupant. The torque box 152, which can be used with both electric and non-electric type headrests, prevents this from happening because the torque box 152 is attached to each backrest rail 68, 70, as shown in
A seat pan 114 which is positioned on the seat pan articulator 96 has a first and second side 116, 118 spaced apart from and substantially parallel to each other, as shown in
When in a neutral, upright position, as shown in
As can be seen from
A fully horizontal position can be achieved because, as shown in
As shown in
In another embodiment, the invention involves a chair 10 comprised of a base assembly 12, a seat frame 14 located above the base assembly 12, a seat 16 and seat back 18 are attached to the seat frame 14. Additionally, an arm rest 126, as shown in
As shown in
The chair 10, described in accordance with this invention, may be suitable for use as a passenger seat in any vehicle including, without limitation, an aircraft, bus or mobile home. In one embodiment, the top and bottom support frames 128, 130 of the arm rest 126 may be substantially parallel to each other. Furthermore, the guide slot 148 may be in the shape of the letter M, as shown in
In one embodiment, the mounting block 136, as shown in
In one embodiment, the top support frame 128 has a first end 138, and a second end 139. A mounting block 136 is pivotally connected at each of the first and second ends 138, 139. As shown in
When in use, the guide pin 144 is positioned in the nadir of the v-shaped portion of the M-shaped guide slot 148. By lifting up on the arm rest 126, an occupant can lift the guide pin 144 off of the nadir and guide the pin 144 up the slots to the top of the leg portion of the M. The occupant then lowers the arm rest 126 and the guide pin 144 travels down the respective leg of the M to a new, lower position. During this movement, the spring 170 acts as a dampener to prevent various components of the arm rest 126, in particular the bottom support frame 130 and the mounting plate 176 from slamming together.
As can be seen from
The bottom support frame 130, which is attached to the seat frame 14, may be a CNC machined guide and the M-shaped guide slot 148 may be manufactured of plastic-like material, thereby reducing the amount of noise caused by the movement of the arm rest 126.
The structure of the arm rest 126 allows for the manufacture of arm rests 126 having various profiles as one is able to vary the height of the support brackets 140 in order to adjust the angle of the top support frame 128. This is accomplished by pivoting the mounting block 136 about its attachment point 172 in the opening or slot 174 in the top support frame 128, as shown in
Because, in one embodiment, the sides of the top support frame 128 extend beyond the top surface, as shown in
All references, including publications, patent applications, and patents, cited herein are hereby incorporated by reference to the same extent as if each reference were individually and specifically indicated to be incorporated by reference and were set forth in its entirety herein.
The use of the terms “a” and “an” and “the” and similar referents in the context of describing the invention (especially in the context of the following claims) are to be construed to cover both the singular and the plural, unless otherwise indicated herein or clearly contradicted by context. Recitation of ranges of values herein are merely intended to serve as a shorthand method of referring individually to each separate value falling within the range, unless otherwise indicated herein, and each separate value is incorporated into the specification as if it were individually recited herein. All methods described herein can be performed in any suitable order unless otherwise indicated herein or otherwise clearly contradicted by context. The use of any and all examples, or exemplary language (e.g., “such as”) provided herein, is intended merely to better illuminate the invention and does not pose a limitation on the scope of the invention unless otherwise claimed. No language in the specification should be construed as indicating any non-claimed element as essential to the practice of the invention.
Preferred embodiments of this invention are described herein, including the best mode known to the inventors for carrying out the invention. It should be understood that the illustrated embodiments are exemplary only, and should not be taken as limiting the scope of the invention.
|Patente citada||Fecha de presentación||Fecha de publicación||Solicitante||Título|
|US1703606 *||3 Nov 1926||26 Feb 1929||Barraket Jacob A||Collapsible chair|
|US3106065 *||13 Feb 1961||8 Oct 1963||Parker Hannifin Corp||Position hold and release mechanisms for flow control valves|
|US3343871 *||3 Mar 1966||26 Sep 1967||George H Yates||Automatically operated invalid chair|
|US3880462 *||30 Ene 1974||29 Abr 1975||Mednick Philip||Reclining chair|
|US4375300||20 Nov 1980||1 Mar 1983||Uop Inc.||Framing system for aircraft passenger seat|
|US4718719||5 Ago 1986||12 Ene 1988||Ptc Aerospace Inc.||Energy absorbing aircraft seat frame structure|
|US4756502||26 Jun 1986||12 Jul 1988||Nordam||Aircraft seat|
|US5018696||26 Abr 1990||28 May 1991||Hoover Universal, Inc.||Power seat adjuster with floating drive mechanism|
|US5485976||12 Ene 1994||23 Ene 1996||Weber Aircraft, Inc.||Plastic bottom diaphragm for aircraft seat|
|US5558309||16 Dic 1994||24 Sep 1996||Societe Industrielle Et Commerciale De Materiel Aeronautique||Convertible structure comprising a plurality of adjacent seats and of variable size along a sliding axis|
|US5568960||15 Sep 1995||29 Oct 1996||Aircraft Modular Products, Inc.||Aircraft passenger seat swivel assembly|
|US5636898||5 Dic 1995||10 Jun 1997||Burns Aerospace Corporation||Seat with recline linkage|
|US5636901||15 Jun 1995||10 Jun 1997||Aircraft Modular Products, Inc.||Aircraft passenger seat frame|
|US5651514||15 Jun 1995||29 Jul 1997||Aircraft Modular Products, Inc.||Recline safety lock assembly|
|US5681091||15 Jun 1995||28 Oct 1997||Aircraft Modular Products, Inc.||Aircraft seat pan assembly|
|US5795025||30 Ago 1996||18 Ago 1998||Aircraft Modular Products, Inc.||Retractable armrest for an aircraft seat|
|US5823614 *||17 Nov 1997||20 Oct 1998||L&P Property Management Company||Three-way reclining furniture item|
|US5836547||8 Abr 1996||17 Nov 1998||Aircraft Modular Products, Inc.||Attenuated seat back assembly for an aircraft passenger seat|
|US5868472||10 Jun 1997||9 Feb 1999||Grilliot; Ronald||Aircraft passenger seat frame|
|US5904407||28 Oct 1997||18 May 1999||Aircraft Modular Products, Inc.||Aircraft seat pan assembly|
|US5954401||30 Ago 1997||21 Sep 1999||Aircraft Modular Products, Inc.||Reclining seat and ottoman system for aircraft including amenity cabinet|
|US5975636||10 Ago 1998||2 Nov 1999||Koch; Roger||Assembly for filling void between cushions of reclining seats|
|US6003927||21 Mar 1997||21 Dic 1999||Mercedes-Benz Ag||Center console having lengthwise, laterally and vertically moveable armrest for an automobile|
|US6305644||14 Ene 2000||23 Oct 2001||B E Aerospace, Inc.||Aircraft cabin seat configuration with enhanced ingress/egress|
|US6352309||13 Ene 2000||5 Mar 2002||Be Aerospace, Inc.||Passenger sleeper seat|
|US6478256||21 Nov 2001||12 Nov 2002||B E Aerospace, Inc.||Passenger seat with seat back breakover assembly and method|
|US6494536||12 Ene 2001||17 Dic 2002||B E Aerospace, Inc.||Passenger seat with variable length seat bottom|
|US6505890||7 Feb 2001||14 Ene 2003||Am-Safe, Inc.||Aircraft seat structure|
|US6604791 *||5 Abr 2002||12 Ago 2003||Hsin Hao Health Materials Co., Ltd.||Reclining leisure chair|
|US6619750||2 Jul 2001||16 Sep 2003||Tachi-S Co., Ltd.||Seat cushion frame for vehicle seat|
|US6644738||21 Nov 2001||11 Nov 2003||B E Aerospace, Inc.||Aircraft passenger seat frame construction|
|US6669143||27 Nov 2002||30 Dic 2003||B E Aerospace, Inc.||Non-encroaching aircraft passenger seat|
|US6669295||21 Nov 2001||30 Dic 2003||B E Aerospace, Inc.||Passenger seat with low profile seat back recline locking assembly|
|US6692069||19 Jul 2002||17 Feb 2004||B E Aerospace, Inc.||Aircraft sleeper seat|
|US6695406 *||12 Ene 2001||24 Feb 2004||Be Aerospace, Inc.||Passenger seat with fabric suspension legrest|
|US6698836||26 Ago 2002||2 Mar 2004||Aviointeriors S.P.A.||Mechanism to obtain the complete reclining of a seat, particularly for an aircraft seat|
|US6742842||3 Jul 2002||1 Jun 2004||B E Aerospace, Inc.||Passenger seat with privacy shell|
|US6749266||21 Nov 2001||15 Jun 2004||B E Aerospace, Inc.||Locking collar for passenger seat back recline assembly|
|US6799805||27 Nov 2002||5 Oct 2004||Be Aerospace, Inc.||Single beam aircraft passenger seat|
|US7040701 *||24 Ene 2002||9 May 2006||Hirofumi Tada||Reclining device|
|US20030111888||18 Dic 2002||19 Jun 2003||Brennan Edward J.||Vehicle passenger seat|
|US20040100138||27 Nov 2002||27 May 2004||Johnson Glenn A||Aircraft passenger seat with forward arm rest pivot|
|Patente citante||Fecha de presentación||Fecha de publicación||Solicitante||Título|
|US8376458||2 Nov 2009||19 Feb 2013||B/E Aerospace, Inc.||Seat pan cam follower with drop down mechanism|
|US9051053 *||10 Ene 2013||9 Jun 2015||Textron Innovations, Inc.||Seat base for aircraft|
|US20140191081 *||10 Ene 2013||10 Jul 2014||Cessna Aircraft Company||Seat Base For Aircraft|
|WO2011053689A1 *||28 Oct 2010||5 May 2011||B/E Aerospace, Inc.||Seat pan cam follower with drop down mechanism|
|Clasificación de EE.UU.||297/316, 297/340|
|Clasificación internacional||B60N2/48, B60N2/68, B60N2/34, B60N2/46, B60N, B60N2/427, A47C7/36, B60N2/22, B60N2/18, B60N2/015, B60N2/00, B64D11/06, A47C7/02|
|Clasificación cooperativa||B60N2/464, B60N2/34, B60N2/4882, B60N2/01508, B60N2/42709, B60N2/4817, B64D11/06, B60N2/18, B60N2/68, B60N2/22, B64D11/064|
|Clasificación europea||B60N2/46C4, B60N2/22, B60N2/48S, B60N2/68, B60N2/48C2B4, B60N2/427D, B60N2/015B, B60N2/34, B60N2/18, B64D11/06|
|14 Ago 2008||AS||Assignment|
Owner name: JPMORGAN CHASE BANK, N.A.,TEXAS
Free format text: SECURITY AGREEMENT;ASSIGNOR:BE AEROSPACE, INC.;REEL/FRAME:021393/0273
Effective date: 20080728
|1 Nov 2010||FPAY||Fee payment|
Year of fee payment: 4
|31 Oct 2014||FPAY||Fee payment|
Year of fee payment: 8
|23 Ene 2015||AS||Assignment|
Owner name: B/E AEROSPACE, INC., FLORIDA
Free format text: RELEASE BY SECURED PARTY;ASSIGNOR:JP MORGAN CHASE BANK, N.A.;REEL/FRAME:034805/0718
Effective date: 20141216
|10 Mar 2015||AS||Assignment|
Owner name: JPMORGAN CHASE BANK, N.A., NEW YORK
Free format text: SECURITY INTEREST;ASSIGNOR:B/E AEROSPACE, INC.;REEL/FRAME:035176/0493
Effective date: 20141216